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Type | Trainer aircraft |
---|---|
First Flight | 1958 |
Primary Users | People's Liberation Army Air Force |
Crew | 2 |
Length | 8.46 m (27 ft 9 in) |
Height | 3.25 m (10 ft 8 in) |
Service Ceiling | 5, 080 m (16, 670 ft) |
Role | Trainer aircraft |
Manufacturer | Nanchang Aircraft Manufacturing Company |
Wing area | 17.0 m² (183 sq ft) |
Max Takeoff Weight | 2, 200 kg |
Powerplant | 1 × Huosai HS-6 radial engine, 285 hp (213 kW) |
Propellers | 2-bladed constant speed propeller |
Cruise Speed | 220 km/h (140 mph, 120 kn) |
Power/Mass | 0.15 kW/kg (0.093 hp/lb) |
Procedure for normal takeoff, including power application, rotation, and initial climb.
Procedure for takeoff with minimum runway length and obstacle clearance.
Procedure for safe takeoff from wet or soft runways at the slowest speed.
Procedure for power-on stall with minimum altitude loss.
Procedure for clean power-off stall with minimum altitude loss.
Procedure for final turn stall with minimum altitude loss.
Procedure for aggravated stall condition with minimum altitude loss.
Procedure for recovering from a normal spin with minimum altitude loss.
Checklists for time-critical emergency actions.